姜权峰1,2, 陈树生1,2(), 杨华1,2, 李祚泰1,2, 高正红1,2
收稿日期:
2023-07-05
修回日期:
2023-07-24
接受日期:
2023-08-11
出版日期:
2024-07-15
发布日期:
2023-08-18
通讯作者:
陈树生
E-mail:sshengchen@nwpu.edu.cn
基金资助:
Quanfeng JIANG1,2, Shusheng CHEN1,2(), Hua YANG1,2, Zuotai LI1,2, Zhenghong GAO1,2
Received:
2023-07-05
Revised:
2023-07-24
Accepted:
2023-08-11
Online:
2024-07-15
Published:
2023-08-18
Contact:
Shusheng CHEN
E-mail:sshengchen@nwpu.edu.cn
Supported by:
摘要:
两级入轨航天器(TSTO)级间分离过程中对轨道级、助推级的姿态精确控制尤为重要。数值模拟可以较为准确地预测级间分离这种飞行器多体分离问题,运用非结构嵌套网格技术及双时间步法耦合流动控制方程、刚体运动方程求解TSTO在攻角-2°、马赫数6、海拔高度30 km的级间分离过程,发展了一种优化轨道级、助推级在级间分离过程的运动姿态的技术。该技术通过松弛迭代法提取轨道级、助推级的无舵偏气动力数据,基于无舵偏气动力数据设计气动舵面、燃气舵所需要提供的俯仰力矩,使得轨道级、助推级的运动姿态更加接近设计目标。数值模拟结果表明,TSTO在分离过程中两级之间会存在强烈的气动干扰,严重影响两级的姿态控制,发展的技术可为TSTO分离过程中轨道级、助推级的舵面运动、燃气舵工作状态设计提供参考,提高TSTO级间分离的效率、安全性。
中图分类号:
姜权峰, 陈树生, 杨华, 李祚泰, 高正红. 两级入轨航天器级间分离姿态精确控制[J]. 航空学报, 2024, 45(13): 129270-129270.
Quanfeng JIANG, Shusheng CHEN, Hua YANG, Zuotai LI, Zhenghong GAO. Precise control of interstage separation attitude of two⁃stage⁃to⁃orbit vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(13): 129270-129270.
1 | 佘文学, 刘晓鹏, 刘凯. 桑格尔空天飞行器技术途径分析与思考[J]. 火箭推进, 2021, 47(6): 11-20. |
SHE W X, LIU X P, LIU K. Analysis and thinking on technical approach of Sanger aerospace vehicle[J]. Journal of Rocket Propulsion, 2021, 47(6): 11-20 (in Chinese). | |
2 | 王长青. 空天飞行技术创新与发展展望[J]. 宇航学报, 2021, 42(7): 807-819. |
WANG C Q. Technological innovation and development prospect of aerospace vehicle[J]. Journal of Astronautics, 2021, 42(7): 807-819 (in Chinese). | |
3 | 王亚军, 何国强, 秦飞, 等. 火箭冲压组合动力研究进展[J]. 宇航学报, 2019, 40(10): 1125-1133. |
WANG Y J, HE G Q, QIN F, et al. Research progress of rocket based combined cycle engines[J]. Journal of Astronautics, 2019, 40(10): 1125-1133 (in Chinese). | |
4 | 苟建军, 肖爽, 胡嘉欣, 等. 高超声速飞行器气动热耗散、输运及转换技术研究进展[J]. 宇航学报, 2022, 43(8): 983-999. |
GOU J J, XIAO S, HU J X, et al. Research progress of aerodynamic heat dissipation,transport and conversion technologies of hypersonic vehicles[J]. Journal of Astronautics, 2022, 43(8): 983-999 (in Chinese). | |
5 | WEINGATNER S. The reference concept of the German hypersonics technology program[C]∥5th International Aerospace Planes and Hypersonics Technologies Conference. Reston: AIAA, 1993. |
6 | 甘才俊, 石伟龙, 李晓辉, 等. 多体模型分离流动的典型气动干扰形式研究[J]. 推进技术, 2023, 44(7): 166-172. |
GAN C J, SHI W L, LI X H, et al. Aero-interference typical patterns for multi-bodies spacious separation flow[J]. Journal of Propulsion Technology, 2023, 44(7): 166-172 (in Chinese). | |
7 | 解福田, 张庆虎, 林敬周, 等. 基于PSP/TSP测量的TSTO标模级间分离气动干扰特性试验分析[J]. 空气动力学学报, 2023, 41(5): 98-108. |
XIE F T, ZHANG Q H, LIN J Z, et al. Experimental analysis of interference characteristics of TSTO stage separation based on PSP/TSP measurement[J]. Acta Aerodynamica Sinica, 2023, 41(5): 98-108 (in Chinese). | |
8 | 林敬周, 解福田, 钟俊, 等. 高超声速风洞双体同步分离捕获轨迹试验技术[J]. 空气动力学学报, 2023, 41(5): 77-86. |
LIN J Z, XIE F T, ZHONG J, et al. Dual-body synchronous captive trajectory test technique in hypersonic wind tunnel[J]. Acta Aerodynamica Sinica, 2023, 41(5): 77-86 (in Chinese). | |
9 | 龚小权, 贾洪印, 赵辉, 等. TSTO级间分离气动特性数值仿真分析[J]. 空气动力学学报, 2023, 41(5): 109-118. |
GONG X Q, JIA H Y, ZHAO H, et al. Numerical simulation analysis on aerodynamic characteristics of TSTO interstage separation[J]. Acta Aerodynamica Sinica, 2023, 41(5): 109-118 (in Chinese). | |
10 | 王粤, 汪运鹏, 王春, 等. 一种并联两级入轨飞行器纵向分离方案的数值研究[J]. 航空学报, 2023, 44(11): 127634. |
WANG Y, WANG Y P, WANG C, et al. Numerical study of longitudinal stage separation for parallel-staged two-stage-to-orbit vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(11): 127634 (in Chinese). | |
11 | 王粤, 汪运鹏, 姜宗林. 激波风洞TSTO纵向级间分离试验技术研究[J]. 航空学报, 2023, 44(20): 128126. |
WANG Y, WANG Y P, JIANG Z L. Research on the test technology of longitudinal stage separation for TSTO in shock tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(20): 128126 (in Chinese). | |
12 | WANG Y, WANG Y P, JIANG Z L. Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle[J]. Physics of Fluids, 2023, 35(5): 056120. |
13 | WANG Y, WANG Y P, JIANG Z L. Numerical investigation of aerodynamic separation schemes for two-stage-to-orbit-like two-body system[J]. Aerospace Science and Technology, 2022, 131: 107995. |
14 | WANG Y, WANG Y P, WANG C, et al. Numerical investigation on longitudinal stage separation of spiked two-stage-to-orbit vehicle[J]. Journal of Spacecraft and Rockets, 2022, 60(1): 215-229. |
15 | LIU Y, QIAN Z S, LU W B, et al. Numerical investigation on the safe stage-separation mode for a TSTO vehicle[J]. Aerospace Science and Technology, 2020, 107: 106349. |
16 | 范孝华, 张庆虎, 罗磊, 等. TSTO并联分离激波/边界层干扰流动特性分析[J]. 空气动力学学报, 2023, 41(5): 87-97. |
FAN X H, ZHANG Q H, LUO L, et al. Flow-field characteristics analyses on shock-wave/boundary-layer interaction of TSTO parallel separation[J]. Acta Aerodynamica Sinica, 2023, 41(5): 87-97 (in Chinese). | |
17 | CHENG J M, CHEN R Q, QIU R F, et al. Aerothermodynamic study of two-stage-to-orbit system composed of wide-speed-range vehicle and rocket[J]. Acta Astronautica, 2021, 183: 330-345. |
18 | SPALART P, ALLMARAS S. A one-equation turbulence model for aerodynamic flows[C]∥30th Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1992. |
19 | ROE P L. Approximate Riemann solvers,parameter vectors,and difference schemes[J]. Journal of Computational Physics, 1997, 135(2): 250-258. |
20 | JAMESON A, YOON S. Lower-upper implicit schemes with multiple grids for the Euler equations[J]. AIAA Journal, 1987, 25(7): 929-935. |
21 | HEIM E R. CFD wing/pylon/finned store mutual interference wind tunnel experiment[R]. Air Force Test Center: Arnold Engineering Development Center, 1991. |
22 | 袁亚. 带头罩折叠翼飞行器多体分离数值模拟[D]. 北京: 中国航天科技集团公司第一研究院, 2017: 20-24. |
YUAN Y. Numerical simulation of multi-body separation of vehicle with shroud and folded wing[D]. Beijing: China Academy of Launch Vehicle Technology, 2017: 20-24 (in Chinese). | |
23 | OPALKA K O. Force tests of the hypersonic ballistic standard models HB-1 and HB-2[M]. Maryland: Ballistic Research Laboratories, 1966. |
24 | 胡守超, 庄宇, 李贤, 等. 高超声速气动热标模HyHERM-Ⅰ试验[J]. 航空学报, 2022, 43(S2): 727804. |
HU S C, ZHUANG Y, LI X, et al. Hyherm-ⅰ test of hypersonic aerodynamic thermal standard model[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(S2): 727804 (in Chinese). | |
25 | 张婷婷, 叶瑞, 姜维, 等. 高超声速风洞HSCM系列标准模型气动力实验数据[J]. 气体物理, 2021, 6(4): 57-65. |
ZHANG T T, YE R, JIANG W, et al. Aerodynamic test data of HSCM calibration models in hypersonic wind tunnel[J]. Physics of Gases, 2021, 6(4): 57-65 (in Chinese). | |
26 | 中国人民解放军总装备部. 高超声速风洞气动力试验方法: [S]. 北京: 总装备部军标出版发行部, 2002. |
General Armament Department. GJB4399-2002 aerodynamics tests method of hypersonic wind tunnel[J]. Beijing: General Armament Department Military Standard Publishing Department, 2002 (in Chinese). | |
27 | 陈树生, 张兆康, 李金平, 等. 一种宽速域乘波三角翼气动布局设计[J]. 航空学报, 2023, 44(23): 128441. |
CHEN S S, ZHANG Z K, LI J P, et al. Wide-speed aerodynamic layout adopting waverider-delta wing[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(23): 128441 (in Chinese). | |
28 | FENG C, CHEN S S, YUAN W, et al. A wide-speed-range aerodynamic configuration by adopting wave-riding-strake wing[J]. Acta Astronautica, 2023, 202: 442-452. |
29 | 唐伟, 刘深深, 余雷, 等. 用于级间分离研究的TBCC动力TSTO气动布局概念设计[J]. 空气动力学学报, 2019, 37(5): 698-704,721. |
TANG W, LIU S S, YU L, et al. Conceptual design of TBCC based TSTO configurations for stage seperation investigation[J]. Acta Aerodynamica Sinica, 2019, 37(5): 698-704, 721 (in Chinese). | |
30 | 李绍磊, 郑建靖, 尚萌萌. 基于非结构网格的飞行器多体分离数值模拟[J]. 计算机应用, 2016, 36(6): 1741-1744,1756. |
LI S L, ZHENG J J, SHANG M M. Numerical simulation of flight vehicle multi-body separation based on unstructured mesh[J]. Journal of Computer Applications, 2016, 36(6): 1741-1744,1756 (in Chinese). | |
31 | 靳晨晖, 王刚, 王泽汉. 子母弹多体分离过程的非定常CFD/RBD数值仿真[J]. 气体物理, 2018, 3(4): 47-63. |
JIN C H, WANG G, WANG Z H. Numerical simulation of unsteady CFD/RBD in multibody separation process of cluster munitions[J]. Physics of Gases, 2018, 3(4): 47-63 (in Chinese). | |
32 | 袁亚, 李冬, 马友林, 等. 基于非结构嵌套网格的低空大动压头罩分离数值模拟[J]. 导弹与航天运载技术, 2019(5): 17-22. |
YUAN Y, LI D, MA Y L, et al. Numerical simulation of shroud separation with overset unstructured grid in low altitude with high dynamic pressure[J]. Missiles and Space Vehicles, 2019(5): 17-22 (in Chinese). | |
33 | LEMMI G, GIACCHERINI S, MARCONCINI M,et al. Application of an overset grid method for the performance analysis of flapping airfoils[J]. Journal of Physics: Conference Series, 2022, 2385(1): 012121. |
34 | XIAO T H, ZHI H L, DENG S H, et al. Enhancement on parallel unstructured overset grid method for complex aerospace engineering applications[J]. Chinese Journal of Aeronautics, 2023, 36(1): 115-138. |
35 | 孔倩. 松弛迭代算法的加速方法研究[D]. 成都: 电子科技大学, 2019: 1-3. |
KONG Q. A study of accelerated technology of relaxation iterative algorithm[D].Chengdu: University of Electronic Science and Technology of China, 2019: 1-3 (in Chinese) . | |
36 | 陈静, 吕玉超, 王利敏. 一种快速收敛的动态松弛协同优化方法[J]. 系统仿真学报, 2018, 30(1): 96-104. |
CHEN J, LÜ Y C, WANG L M. Dynamic relaxation cooperative optimization method with fast convergence[J]. Journal of System Simulation, 2018, 30(1): 96-104 (in Chinese). |
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